Boeing 727-224

Service difficulty reports · 2,252

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727224'
  ORDER BY difficulty_date DESC"

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SDR DHL2007746501Seat Track · corrodedSURFACE CORROSION OVER LENGTH OF SEAT TRACK BS 680-740 RBL24. REMOVED DAMAGED SEAT TRACK SECTION IAW B727 SRM 51-30-2 AT RBL 24.75 FROM STA 680-740 IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW B727 SRM 53-10-5 FIG1 AND 53-10-2 FIAug 22, 2007 · N746DH · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007746535Shear Tie · corrodedAFT CARGO COMPT BS, 950 A O/B AT STR 29 RT, LOWER FRAME HAS EXFOLIATING CORROSION. REMOVED SHEAR TIE AT AFT CARGO COMPT IAW B-727 SRM 51-30-2. FABRICATED SHEAR TIE, MAT USED BAC 1505-29222, 7075-T6, PO NR 9004670, DIMENSION 7", IAW.B-727. SRM 53-10-2, FIG-5 Aug 21, 2007 · N746DH · Boeing 727224 · Fuselage Internal Mounting StructureSDR DHL2007746536Intercostal · corrodedAFT CARGO COMPT BS 950F-970 INTERCOSTAL AT STRINGER 28 LT IS CORRODED. REMOVED INTERCOSTAL IAW B-727, SRM 51-30-2. FABRICATED NEW INTERCOSTAL, MAT USED 7075 T6, 0.040, PO NR 9005634, DIMENSION 20" BY 7 1/2 IAW B-727, SRM, 53-10-2, FIG-5 AND 51-10-3, AND 51-3Aug 21, 2007 · N746DH · Boeing 727224 · Fuselage Miscellaneous StructureSDR DHL2007746524Stiffener · corrodedC-1 DOOR LOWER STIFFENERS AND FRAMES CORRODED ABOVE LOWER FRAME BODY STATION 560-620. REMOVED LOWER STIFFENERS AND FRAME AT C1 DOOR IAW B727 SRM 51-30-2. FABRICATED TWO TEE SUPPORT DIMENSION 9 3/4 EACH MATERIAL USED BAC1505-29222 7075T6 PO NR 9004174 AND FABAug 21, 2007 · N746DH · Boeing 727224 · Cargo/Baggage DoorsSDR DHL2007746503Skin · chafedAT C CHECK RT INBD FORE FLAP L/E WBL 124 IS CHAFED ON REPAIR AND ADJACENT SKIN. REMOVED PREVIOUS REPAIR AT RT INBD FORE FLAP L/E WBL 124 IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR MATERIAL USED 7075-T6 .050 PO NR 9005314 DIM 4" BY 4" IAW B727 SRM 57-50-2 FIAug 21, 2007 · N746DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2007746504Frame · crackedWHILE AT FLIGHTSTAR FOR A C CHECK,N/R 099359 DISCREPANCY: HOLE DRILLED IN RADIUS OF FRAME BS 700 STR17R. CUTOUT DAMAGED AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG. FABRICATED ANGLE REPAIR FROM 7075T6 .O50 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1, 53-10-2 FIAug 20, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746502Frame · damagedWHILE AT FLIGHTSTAR AIRCRAFT SERVICES FOR A C CHECK, N/R 099360 DOUBLER DRILLED HOLES IN FRAME BS 680 STR 17R. CUTOUT DAMAGED AREA DIM 1" BY 1" IAW B727 SRM 51-40-3 FIG 1. FABRICATED ANGLE REPAIR FROM 7075 T6 .050 DIM 9" BY 4" IAW B727 SRM 53-10-2 FIG3 AND 5Aug 20, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746521Stringer · corrodedWHILE AT FLIGHTSTAR FOR A "C" CHECK, FWD CARGO COMPT STR 26L IS CORRODED AT STA 740. CUT OUT DAMAGE SECTION OF STR 26LT AT STA 740 IAW B727 SRM 53-10-03, 5" LONG FAB AND INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-03 FIG 1, MAT USED STRINGER BAC1498-147 7075Aug 18, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746507Skin · corrodedDURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED: SURFACE CORROSION ON BS 720D STR 27R ON SKIN. CUT OUT DAMAGED AREA ON SKIN AT STA 720D STR 27R IAW B727 SRM 53-30-3 FIG 3 4 3/4 BY 4". FABRICATED AND INSTALLED REPAIR DOUBLER IAW B727 SRM 53-30-3 FIAug 15, 2007 · N746DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR GAIA07013OPLight · inoperativeNO FLIGHT: DURING A CHECK, FOUND L-1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. AC WAS RETURNED TO SERVICE. (K)Aug 14, 2007 · N69735 · Boeing 727224 · Emergency LightingSDR DHL2007746511Frame · corrodedWHILE AT FLIGHTSTAR FOR A "C" CHECK, FUSE BS 303.9 FRAME AT LT WALKWAY BEAM HAS EXFOLIATED CORROSION WL 143. CUT OUT DAMAGED AREA OF FRAME AT LT WALKWAY BEAM NWW AREA BS 303.9 WL 143 IAW B727 SRM 51-10-4 FIG 5. FABRICATED AND INSTALLED DOUBLER REPAIRS IAW B7Aug 13, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746506Intercostal · corrodedDURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 099407, AFT CARGO COMPT AT BS 950A OB OF STR 28R INTERCOSTAL LWR FLANGE HAS EXFOLIATED CORROSION. REMOVED AFT BODY PANEL NR 3522 IAW B727 SRM 51-30-2. REMOVED INTERCOSTAL AT AFTAug 10, 2007 · N746DH · Boeing 727224 · Fuselage Miscellaneous StructureSDR DHL2007746522Stringer · corrodedWHILE AT FLIGHTSTAR FOR A "C' CHECK, AFT CARGO COMPT BS 950F-970 STR 28L HAS CORROSION O/B SIDE. CUTOUT DAMAGED AREA DIM 36" IAW B727 SRM 53-10-03 FIG 1, FAB STR REPAIR DIM. 36" MAT. USED BAC1498-145 7075-T6 PO NR 9004219. FAB 3 SPLICE MAT USED BAC1498-131 Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746520Stringer · corrodedWHILE AT FLIGHTSTAR FOR A "C" CHECK, FWD CARGO COMPT, STA 685 STR SPLICE HAS CORROSION IN CENTER OF SPLICE STR 28LT. REMOVED STRINGER SPLICE AT STR 28 LT STA 680 IAW B-727 SRM 51-30-2 FIG-1. FABRICATED NEW SPLICE FROM BAC 1498-131 7075T6, PO NR 7232174 DIM 1Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746519Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, FUSELAGE FRAME DENTED BS 640 BETWEEN 16R-17R. CUT OUT DAMAGE AREA DIM 1.5" AND 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB ANGLE REPAIR FROM 7075-T6 .050 PO NR 9005138 IAW B727 SRM 53-10-02 AND 51-40-03 FIG 1, LOCATED AND DAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746518Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 540 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746517Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 520 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746516Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 500 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1, FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILLAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746515Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 480 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 1. FAB DOUBLER ANGLE. REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LOCATED DRILAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746514Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 600 BETWEEN STR 16R-17R. CUT OUT DAMAGE AREA, DIM 1" BY 1" IAW B727 SRM 51-40-03 FIG 6. FAB DOUBLER ANGLE REPAIR FROM 7075-T6 .050 PO NR 9003230 DIM 9" BY 4" IAW B727 SRM 51-40-03 FIG 1. LEATED Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746513Frame · dentedWHILE AT FLIGHTSTAR FOR A "C" CHECK, DENT ON FUSELAGE FRAME BS 580 ABOVE STR 17R. CUT OUT DAMAGE AREA DIM 1" BY 1" IAW B727 SRM 51-40-03. FAB DOUBLER ANGLE REPAIR DIM 9" BY 4" FROM 7075-T6 .050 PO NR 9003230 IAW B727 SRM 51-40-03 FIG 1 AND LOCATED DRILL IAW Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2007746508Stringer · corrodedDURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED; REF NR 099303, FWD CARGO COMPT STA 685 STR. SPLICE HAS CORROSION IN CENTER OF SPLICE STR 27L. ALSO CRACK INDICATION. REMOVED STRINGER SPLICE AT STR 27L STA 680 IAW B727 SRM 51-30-2 FIAug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746505Stringer · corrodedDURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 099305. FWD CARGO COMPT STA 685 STR 27R HAS CORROSION IN CENTER OF SPLICE. REMOVED STRINGER SPLICE AT STR 27R STA 680 IAW B727 SRM 51-30-2 FIG 1. FAB NEW SPLICE FROM BAC 1498-131,7075 T6 PO Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL200774650Stinger · corrodedDURING A "C" CHECK AT FLIGHTSTAR, THE FOLLOWING DISCREPANCIES WERE NOTED REF NR 099305, FWD CARGO COMPT STA 685 STR 27R HAS CORROSION IN CENTER OF SPLICE. REMOVED STRINGER SPLICE AT STR 27R STA 680 IAW B727 SRM 51-30-2 FIG 1. FAB NEW SPLICE FROM BAC 1498-131Aug 9, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746512Stringer · crackedWHILE AT FLIGHTSTAR FOR A "C" CHECK, STRINGER 15L CRACKED AT BS 720B+15. STRIPPED PAINT FROM AREA IAW B727 MM 51-20-01, CUT OUT DAMAGE AREA DIM 13" IAW B727 SRM 53-10-03 FIG 1. AFTER NOT VERIFIED CRACK FAB STRINGER FROM BAC2798-143 7075-T6 PO NR 7267138 DIM Aug 7, 2007 · N746DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHL2007746509Tab · crackedDURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT OUTBD AILERON BALANCE TAB, LEADING EDGE CENTER HAS A CRACK. REF NR 099154, REMOVED DAMAGED SECTION OF LT O/B AILERON BALANCE TAB L/E CENTER IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED NEW SECAug 6, 2007 · N746DH · Boeing 727224 · AileronsSDR DHL2007746510Cowling · damagedDURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED, REF NR 098958 NR 1 ENG NOSE COWL EXTERIOR SKIN AT 9 O'CLOCK POSITION HAS 3 INCH CRACK FROM RIVET HEAD FWD. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL EXTERIOR SKIN 9 O`CLOCK POSITION 3" BY 2" IAW B7Aug 3, 2007 · N746DH · Boeing 727224 · Nacelle/Pylon, Main FrameSDR GAIA0709Servo · inoperativeON DOWN WIND LEG TO LANDING WITH THE AUTO PILOT ON THE FLIGHT CREW TURNED THE YOKE LEFT AND RIGHT WITH NO MOVEMENT OF THE AIRCRAFT. A RATCHETING SOUND WAS OBSERVED. THE AUTO PILOT WAS TURNED OFF AND THE CONDITION CONTINUED FOR 1 MINUTE THEN NORMAL OPERATION Jul 26, 2007 · N69735 · Boeing 727224 · Autopilot Main ServoSDR DHL2007745004Engine · malfunctionedNR 2 ENGINE N1 GAUGE FLUCTUATED RAPIDLY FINALLY WENT TO 0 NR 2 ENGINE OIL TEMP IN YELLOW. C/W ABNORMAL PROCEDURES INFLIGHT SHUTDOWN. COMPLETED OIL TEMP IN YELLOW ARC PRIOR TO ABOVE PROCEDURE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.1.Jan 18, 2007 · N745DH · Boeing 727224 · Engine (Turbine/Turboprop)SDR DHL2007747001Skin · gougedRT INBD FORE FLAP O/B LEADING EDGE HAS GOUGE ON REPAIR DOUBLER. REMOVED AND REPLACED DAMAGED REPAIR FROM RT INBD FORE FLAP O/B LEADING EDGE IAW B727 SRM 57-50-4.Jan 5, 2007 · N747DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006754003Compressor · stalledON T/O AT ILN, REJECTED T/O AT 60 KTS, COMPRESSOR STALL NR 2 ENG AUTO PACK TRIPPED. RESET PACKS. RAN CHECKLIST. ALL INDICATIONS NORMAL. NORMAL T/O ON SECOND ATTEMPT. CREW ADVISED MTX THAT THERE WAS 20+ MPH CROSSWINDS, PERFORMED INLET AND EXHAUST VISUAL INDec 1, 2006 · N745DH · Boeing 727224 · Turbine Engine Compressor SectionSDR DHL2006746005Attach Angle · crackedCRACK FOUND IN LEFT WING BELOW NR 7 SPOILER IN THE RADIUS OF THE ATTACH ANGLE COMMON TO SPOILER ACTUATOR FITTING, APPROX WBL 124.2, CRACK LENGTH APPROX 1.5". REMOVED LOWER CHORD PREVIOUS REPAIR AND DOUBLERS PER B727 SRM 51-30-2. FABRICATED NEW CHORD FROM BACNov 21, 2006 · N746DH · Boeing 727224 · Wing Miscellaneous StructureSDR DHL2006746004Control System · malfunctionedENTRY DOOR EMERGENCY EXIT LIGHT ILLUMINATED DURING LANDING. SECURED CONTROL CABIN EMERGENCY EXIT LIGHT. OPS OK PER B727, MM CH 33-50-01.Nov 1, 2006 · N746DH · Boeing 727224 · Emergency LightingSDR DHL2006746003Indicator · malfunctionedAT BEGINNING OF TAKE-OFF ROLL, TAKE-OFF THRUST SET, MACH AIRSPEED WARNING SOUNDED. INDICATED AIRSPEED LESS THAN 60 KTS. REMOVED AND REPLACED FO'S MACH AIRSPEED INDICATOR IAW B727 MMS CH 34-12-21. TESTS GOOD. PITOT/STATIC TEST GOOD IAW B727 MMS 34-11-00. REMOVOct 5, 2006 · N746DH · Boeing 727224 · Airspeed/Mach IndicatorSDR DHL2006747003Battery · no testCOCKPIT EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED LIGHT ASSY. BATTERIES, OPS CK. NORMAL IAW BMM REF 33-50-01. P/N 37067-001.Sep 19, 2006 · N747DH · Boeing 727224 · Emergency LightingSDR DHL2006745543Stringer · crackedREF ASTAR N/R 56475. LT WING NR 1 FUEL TANK INTERIOR UPPER WING STR 10 IS CRACKED WHERE ATTACH TO RIB AT WS 656.5 REMOVED FASTENERS AT LWS 656.5, STR 10 FOR REPAIR AND NDT VERIFICATION OF CRACK IAW SRM 51-30-2, C/W HFEC IAW NDTM, PT 6, 51-00-00 FIG 23, VERIFSep 16, 2006 · N745DH · Boeing 727224 · Wing, Longeron/StringerSDR DHL2006745541Spar · tool damageREF ASTAR N/R 56628. RT HORZ STAB LWR AFT REAR SPAR CHORD (75 PERCENT CHORD) FROM ELEV STA 45.5 TO 140 HAS MISDRILLED SEAL HOLES, MISSING FASTENERS AND SEAL LOOSE IN SEVERAL PLACES. CUT OUT DAMAGED AREA AT RT HORIZ STAB LWR AFT REAR SPAR CHORD APPROX DIM 1.5 Sep 16, 2006 · N745DH · Boeing 727224 · Horizontal Stabilizer, Spar/RibSDR DHL2006745539Skin · corrodedEXFOLIATING CORROSION FOUND AT L2 DOOR FUSE CUTOUT, AFT SIDE, BS 1068, WL 239.0, AS MARKED. REMOVED FASTENERS AT L2 DOOR CUT OUT BS 1068, WL 239 IAW B727 SRM 51-30-2. REMOVED CORROSION BY L2 DOOR CUTOUT IAW B727 SRM 51-10-6, CORROSION FOUND OUT OF LIMITS IAWSep 16, 2006 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHL2006745538Seat Track · corrodedCABIN SEAT TRACK BS 980, RBL 25 HAS CORROSION AS MARKED. REMOVED & REINSTALLED FLOORBOARD AFTER FAB SEAT TRACK FROM BS 950E TO 1060, RBL 24. REMOVED SEAT TRACK & FAB NEW FROM P/N BAC 1520-792, PO 9003091 DIM 103", TREATED, PRIMED, & INSTALLED NEW FAB SEAT TRSep 13, 2006 · N745DH · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006745537Wedge · delaminatedREF ASTAR N/R 55925. DISCREPANCY: RT O/B FORE FLAP SHOW DELAM SPOT T/E IB END, WBL 298. REMOVED END CAP AND REMOVED DAMAGED UPPER AND LOWER SKINS, CORE, AND WEDGE; FABRICATED REPAIR CORE, 2 EA SKINS AND 2 EA DOUBLERS. BONDED LOWER REPAIR SKIN, DOUBLER AND Sep 9, 2006 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHL2006745533Support Fitting · crackedREF ASTAR N/R 56236. AFT STAIR RT WEEL AREA BS 1263 TORQUE BOX ANGLE CRACK INDICATION, LWR OF ACTUATOR FITTING SUPPORT. REMOVED FASTENERS AND SHIM AT BS 1263, IAW SRM 51-30-2. PERFORMED HFEC IAW D6-48875, PART 6, 51-00-00 FIG 23 TO CONFIRM CRACK, CRACK CONFISep 9, 2006 · N745DH · Boeing 727224 · Fuselage Main, Attach FittingsSDR DHL2006745542Attach Angle · crackedASTAR N/R 073041-LT WING NR 1 FUEL TANK INTERIOR UPPER, STR-10 CRACK INDICATION FROM WHERE ATTACH TO RIB AY WS 686.5. CRACK END AT FASTENER HOLE. NDT CONFIRMED. REMOVED FASTENERS AT WS 686.5 STR. 10 FOR REPAIR IAW SRM 51-30-2,DRILLED AND TRIMMED REPAIR ANGLESep 8, 2006 · N745DH · Boeing 727224 · Wing, Attach FittingsSDR DHL2006745534Intercostal · corrodedFWD CARGO COMPT, INTERCOSTAL IS CORRODED ON BOTH SIDES BETWEEN STA 680-700, LBL 1. REMOVED INTERCOSTAL FROM BS 680-700, LBL 1, FOUND TO BE OUT OF LIMITS. FAB NEW INTERCOSTAL FROM 7075-0, .050", PO 9003137, DIM 20" X 8.5. HEAT TREATED TO T6 CONDITION IAW FLISep 8, 2006 · N745DH · Boeing 727224 · Fuselage Miscellaneous StructureSDR DHL2006745530Seat Track · corrodedMAIN CARGO DECK 45R SEAT TRACK AT BS 950 SHOWS SURFACE CORROSION. REMOVED CORRODED SEAT TRACK BS 950-1030, RBL 45 IAW B727 SRM 51-30-2, FAB NEW SEAT TRACK FROM P/N BAC1520-792, PO 9003091APPROX DIM 16' IAW B727 SRM 53-10-5 FIG 1 & SRM 53-10-2 FIG 7, FAB REPAISep 8, 2006 · N745DH · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006745523Frame · dentedFWD CARGO COMPT, FRAME AT STA 640 IS DENTED AT UPPER FLANGE ABOVE STR 24R. CUT OUT DAMAGED SECTION 1" BY 1" AT FWD CARGO FRAME BS 640 UPPER FLANGE ABOVE STR 24R IAW B727 SRM 51-40-3 FIG 1, FAB DOUBLER FROM P/N 7075-0 .050, PO NR 9003749, APPROX DIM 8" BY 4" ISep 5, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745536Frame · dentedAFT CARGO COMPARTMENT LT STA 1110 HAS DENT IN RADIUS OF FRAME. CUT OUT DAMAGED SECTION DIM, 2 EA, 1 1/2" BY 1" AND 1" BY 3/8" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR USING 7075-0, .071", PO NR 9003189, DIM 22" BY 5" IAW B727 SRM 53-10-2, HEAT TRESep 2, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745524Frame · dentedAFT CARGO COMP BS 1070 ABOVE STR 26R HAS FRAME INNER CHORD DENTED. CUT OUT DAMAGED AREA APPROX DIM 3/4" BY 1" IAW B727 SRM 51-40-3 FIG 1, FAB REPAIR DOUBLER FROM 7075-0 .063" PO NR 9003418 APPROX DIM 7 1/2" BY 3 5/8" IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3Sep 2, 2006 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHL2006745522Window Frame · corrodedFOUND CORROSION ON WINDOW FRAME BS 950C +10" LEFT SIDE. CORROSION ON WINDOW FRAME SKIN WAS FOUND OUT OF LIMITS, MATERIAL REMOVED .008" IAW B727 SRM 56-20-1. REMOVED FASTENERS IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER USING 2024 T3, .160", PO NR 614918Sep 2, 2006 · N745DH · Boeing 727224 · Fuselage Main, StructureSDR DHL2006745544Intercostal · tool damageFWD CARGO COMPT, INTERCOSTAL HAS DEEP DRILL MARK AT STA 540 +10 INCHES BETWEEN STR 23R AND 24R. REMOVED DAMAGED INTERCOSTAL AT BS 540 + 10 INCHES BETWEEN STR 23R & 24R IAW B727 SRM 51-30-2, FAB NEW INTERCOSTAL FROM P/N 7075-T6, .063, PO 9002695, APPROX DIM 8"Sep 1, 2006 · N745DH · Boeing 727224 · Fuselage Miscellaneous StructureSDR DHL2006745529Frame · dentedREF ASTAR N/R 56325. AFT CARGO COMP BS 1050 ABOVE STR 26R HAS FRAME INNER CHORD DENTED. CUT OUT DAMAGED AREA APPROX DIM .7500 IN X 1INCH IAW SRM 51-40-3 FIG 1, FAB REPAIR DOUBLER FROM P/N 7075-0, .063, PO NR 9003418 APPROX DIM 8 .5 INCH X 3.6250 IAW SRM 51-4Sep 1, 2006 · N745DH · Boeing 727224 · Fuselage Main, Frame
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